Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
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OXIDATION-RESISTANT NICKEL ALLOY
This in~ention relates to nickel base alloys for use in
severe conditions of oxidation and high temperatures, and
more specifically, to nickel base alloys containing chromium,
tungsten and molybdenum as principal elements for optimum
oxidation and engineering properties.
B~CKGROUND
Nickel base superalloys have been developed for use in
severe service conditions including corrosion, high tempera-
ture and mechanical operations. Typical examples include a
group of recent patented a~loys as defined in U S. ~atent
lS Nos. 3,865,581, 45~06,015, 4,110,110 and 4,194,909. 5Omposi-
tions of these alloys are shown in Table 1. Table 1 lists
the broadest ranges of all elements required or optional as
disclosed. The alloys appear to be closely re]ated in composi-
tions. The compositional variations among ~hese alloys,
although seemingly minor, are effective to the extent that
each of the alloys is a distinctive alloy with physical and
mechanical properties especially sui.ted for a particular
use. This situation is geneTally common in metallurgy and
especially in the superalloy arts.
PRIOR ART
U.S. Patent 3,865,581 is especially suited for use at
high temperature and where tcrsional strengtll is required.
The alloy depends upon the relations]lip among boron, magnesium,
beryllium and especially, critical contents of zirconium
S~5S
and cerium for optimum results.
- U.S. Patent 4~006,015 is especially suited for use at
high temperature under conditions requiring good creep-
rupture properties. The alloy contains critical proportions
of nickel, chromium, tungsten and titanium.
U.S. Patent 4,110,110 is especially suited for use in
nuclear applications in low oxidizing atmospheres, for
example, argon or vacuum. The effective properties are
obtained by proper contents of chromium, manganese and
silicon with critical limitations of titanium and aluminum.
U. S. Patent 4,194,909 is especially designed for use
in gas cooled reactors. The desired properties (including
creep rupture) are obtained by the critical control of
calcium, magnesium, zirconium, niobium, hafnium and a rare
earth metal. Further, the alloy must not contain cobalt and
titanium.
The patents appear to disclose a particular group of
related alloys. The basic compositions appear to be generally
similar.
These patents, in general, teach the critical content
of one or more minor elements, inter alia, to achieve
optimum results. The teachings vary, for example, t~hile one
patent teaches a low aluminum content, another discloses a
higher aluminum content as critical. This suggests the "art
and science" of this class of alloys is not established and
needs additional improvements.
OBJECTS OF THIS INVENTION
It is the principal object of this invention to provide
a novel alloy with improvements in a combination of good
engineering properties.
It i5 another object of this invention to provide an
alloy with a high degree of oxidation resistance and high
strength in prolonged elevated temperature enviTOnmentS.
Other aims and objectives will become apparent to ~hose
skille~ in the art in view of subsequent disclosures~
SU~MARY OF THE INVENTION
These and other objects and advantages are obtained by
the provision of the alloy of this invention as described in
Table 2. Contrary to the commonly accepted notion that
tungsten and molybdenum are often interchangeable totally or
in part, the alloy of this invention requires both tungsten
and molybdenum must always be pTeSent, within the ranges
sho~n in Table 2 and in critical proportions. Tungsten must
always exceed molybdenum by a ratio at least about 4.5 to 1,
respectively, within the ranges given in Table 2. Furthermore,
in the alloy of this invention, the contents of chromium,
tungsten and molybdenum must be present in the critical
relationship:
Cr = about 2.05 to 2.65
Mo f 172 W
where Cr = percent chromium by weight
Mo = percent molybdenum by l~eight
~ = percent tungsten by weight
.f~lS
Cr
W:Mo ratio should be about 7:1 and the Mo + l/2 IY ratio
should be within the range 2.2 to 2.6 for optimum benefits
of this invention.
It was discovered, as a critical feature of this
invention, the control of the electron vacancy (Nv) number
is essential to obtain the objectives of this invention. The
method of determining the electron vacancy number is dis-
cussed in The Journal of Metals October, 1966, by C. T. Sims
and U.S. Patent 4,118,223.
For the purposes of this invention, it was found that
the formation of desirable intermetallic precipitates can be
avoided by controlling a balanced composition for which the
Nv has a value of not over 2.5 and prefeTably less than
about 2.4. The Nv numbers for the experimental alloys are
shown in Table 2.
Balancing the composition of the alloy to obtain the
lowest Nv number imposes an additional limitation and burden
in the production of the alloy of this invention. Never-
theless, it is essential to maintain a very low Nv number to
obtain the full benefits of this invention.
Although the exact mechanism of the science of the
invention is not completely understood, it is believed that
the critical amount and ratio of chromium, tungsten and
molybdenum act in a synergistic manner to provide the
valuable combination of oxidation resistance and strengt~.
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These elements appear to be present in a crucial proportion
of carbide formers and in solid solution. Because of this
crucial proportion in the microstructure, the alloy of this
invention resists dynamic oxidation losses and has a high
degree of stress rupture life.
Iron, cobalt, columbium, tantalum, vanadium, zirconium,
and the like are tolerable in the alloy as adventitious
elements as may be found in alloys of this class. Aluminum
may also be present as a result of processing, i.e. deoxida-
tion and adequate control of lanthanum. A content of up to
about .50% aluminum may be present.
Examplec
To verify the advantages of t~e novel alloy, a series
of alloys as described in Table 3 was produced. ~he alloys
contained advertitious contents of cobalt, aluminum, iron,
and other elements normally found in alloys of this class.
The entire composition range of the four alloys was rela-
tively narrow. Test results of these alloys reveal an
unexpected result. Within t}e already narrow range of
compositionJ a critical ratio Mo + 1/2W was discovered
2~ to provide an outstanding combination of valuable proper-
ties. Thus, this invertion resides in the provision of an
alloy with a narrow composition range and a required ratio
among chromium, tungsten and molybdenum. Alloy 13178 is the
alloy representative of this invertion. Subsequen~ data
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and discusslon will show Alloy 13178 to be superior over the
other experimental alloys and that such superiority is
totally unexpected. The values of ~lo ~ 1/2iY for the four
exp~ri~lental alloys range from 1.52 to 2.74, while the
content of all otheI elements remain relatively constant.
Subse~uent data will be presented th~t shows the variation
of properties in teTms of the ~lo + 1/21Y Tatio values. The
data show, in every case, the best combination of proper~ies
is obtained at the ratio value of about 2.2 tc about 2.6.
This is unexpected. It would be expected that, since all
elements are relatively constant, the best alloy s~ould be
the one with the highest or lowest ratio value.
The alloys were prepared by vacuum induction mel~ing
(VIM) then electro-slag remelting (ESR) to refine the
composition.
Each heat was prepare~ as a 4-inch ingot the~ hot
forged to l-inch stock. Following an anneal at 21~0F, the
12.7mm
heats were hot rolled to l/2-inch thick stock at 215DF.
2 5mm
~lh77 ~ ats were then cold rolled tlo30 l-inch, annealed at
2150 F, and coldl2r3o2bced down to 0.05 inch. The flnal anneal
temperature was 2250F followed by rapid cooling.
Because the melting of the alloy of this invention was
relatively trouble-free, it is expected that the alloy may
be produced by most well-known processes. Furthermore,
because the casting and working characteristics of the allo~
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of this inVentioll are relativcly trouble-free, the alloy may
be produced in a great variety o commercial forms including
castings, wires, powders, -~elding and hardfacing product.s
and the like.
TEST RESUI,TS
Test samples of the four experimental alloys were
tested under very severe oxidation conditions. The well-
~. ,
known dynamic oxidation test procedure ~as used as follows:
1.6mm 9.5mm 7S.2mm
1. Prepare specimens about 1/16 ~ 3/8 x 3 inches.
12 ~
2. Grind all surfaces to a 120-grit finish and
de~rease in a solvent such as acetone.
3. Measure exact surface area and weight of each
specimen.
4. Expose specimens in a holder rotating at 30 RP~
to the combustion products of an oil fiTed flame
plus excess air moving at a velocity of about 0.3
Mach.
5. Cool to near ambient temperature each 30 minutes.
6. Weigh each sample after every 25-hours of the test
for the duration of the tests.
50.8mm
7. Section each sample at a point 2-inches from the
base, mount for metallographic examination and
optionally measure depth of continuous penetration,
depth of internal oxidation and unaffected thicXness.
8. Calculate average weight loss (mg/cm2)_
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9. Calculate total depth of affected metal.
F~ure 1 is a graphic present:ation of the metal d~leight loss
data obtained in the dynamic oxidation test at 1800F for
500 hours.
Fi~ure Z is a graphic presentation of the depth of affOected
982 C
metal data obtained in the dynamic oxida*ion test at 1800F
for 500 hours.
Fi~ure 3 is a graphic presentation of the metal Oeight loss
1093 C
data obtained in the dynamic oxidation test at 2000F for
times up to 500 hours. Figure 3 also contains data obtained
for two well-known commercial alloys: Alloy 188 and Alloy X.
Alloy 188 is cobalt-base containing 22% chromium, 22% nickel,
14.5~ tungsten, 0.07% lanthanum. Alloy X is nickel-base
containing 22% chromium, 9% molybdenum and 18.5% iron.
Figure 4 is a graphic presentation of the metal ~ight loss
data obtained in the dynamic oxidation test at 2000F for
300 hours.
Fi~ure 5 is a graphic presentation of the stress-rupture
life data obtained by the standard well-lcnown "Stress
982C
Rupture Test". Data are presented for tests at 1800F and
27.6MPa
4000 psi load.
The data clearly show that both (1~ alloys with higher
ratio values and (2~ alloys with lower ratio values are
inferior to the alloy of this invention, which has a ratio
value of 2.37. The test data suggest that the value of
5~
Cr
~lo + 1¦~ may vary from about 2.2 to about 2.6 and yet
retain the benefits of this invention. This range may be
expected during the commercial production of alloys of this
class. It is not practical to expect to get exact aim points
in every production heat. A reasonable range must be expected.
For this reason, the broad and preferred composition ranges
of the alloy of this invention are suggested.
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TABLE 2
; ALLOY OF THIS INVENTIoN
Composition, wei~ht-percent
; _oad Range Preferred Ran~e Typical Alloy 13178
Al .50 max .50 max .50 max - .06
B .02 max .001 - .015 about .01 .006
C .05 - .15 .05 - .lS about .10 ; .10
Cb .2 max .2 max .2 max ;- ~
Co 5 max 3 max 3 max
Cr 20 - 24 20 - 24 about 22 - 21.40
Fe 5 max 3 max 3 max
LaTrace - .05 .005 - .05 about .02 .021
Mn .3 - 1.0 .3 - 1.0 about .50 .42
~So1.0 - 3.5 1 - 3 abou~ 2.0 2.0
P .03 max .02 max .02 max
S .015 max .008 max .008 max
Si .20 - .75 .20 - .60 about .40 .23
Ta .2 max .2 max .2 max
. Ti .2 max .2 max .2 max `
V .2 max .2 max -.2 max
IY 10 - 20 13 - 15 about 14 14.08
` Zr .2 max .2 max .2 max
; Nï Bal* Bal* Bal*
IY:Mo4.5 to 12:1 5:1 to 10:1 about 7:1 7-04
' Cr
Mo + 1/2W 2.05 - 2.65 2.2 - 2.6 about ~.4 2.~7
*Nickel plus impurities
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In the alloys of the invention, the follow-
ing elements are optional and may be present in amounts
from 0%; Cb, Co, P, S, Ta, Ti, V and Zr.
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